Method presented by which directional stability derivative Cns, rate of change of yawing moment coefficient with sideslip angle, can be evaluated for conventional airplane from flight records of lateral or directional oscillation.
Simplified method for determining from flight data rate of change of yawing-moment coefficient with sideslip
Nat Advisory Committee Aeronautics -- Tech Note
1946
8 pages
4 Supp sheets
Report
English
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Estimation of rate of change of yawing moment with sideslip
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